# Service difficulty reports: N8079U, cancelled Sep 6, 2001

A list on [N8079U, cancelled Sep 6, 2001](https://openairdocs.org/deregistered/N8079U-2001-09-06.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 2 · 84 reports

- [SDR 99T64R545EWA](https://openairdocs.org/sdr/99T64R545EWA.md): Pin Boss · corroded · Nov 19, 1999 · N8079U · Doug DC871 · Landing Gear Retraction/Extension System
  > DURING D-CHECK. LT MAIN GEAR SHOCK STRUT ASSY RETRACT PIN BOSS CORRODED. (EO). BLENDED OUT CORROSION. FABRICATED NEW BUSHING AND CAD PLATED IAW EO 99-174 WITH APPROVED 8110-3 DATED 10-15-99. INSTALLED BUSHING AND PIN IAW DC-8 SB 32-102. REF: EMERY WOR
- [SDR 99T64R533EWA](https://openairdocs.org/sdr/99T64R533EWA.md): Fastener · missing · Nov 13, 1999 · N8079U · Doug DC871 · Wing Miscellaneous Structure
  > FOUND DURING D-CHECK. RT WING L/E ABOVE NR PYLON. ONE LOOSE FASTENER WITH SKIN WASHER, ONE FASTENER MISSING. (EO). TIGHTENED THE LOOSE FASTENER. INSTALLED NAS1670L4 JO-BOLT IN OPEN HOLE. IT IS ACCEPTABLE TO RETURN TO SERVICE PER EO 99-174 WITH APPROVED 8
- [SDR 2000T74R547EW](https://openairdocs.org/sdr/2000T74R547EW.md): Metal Strip · cracked · Nov 12, 1999 · N8079U · Doug DC871 · Nacelle/Pylon Structure
  > DURING C-CHECK. NR 2 ENGINE LT SIDE METAL STRIP ABOVE REVERSER COWL HAS.75 INCH CRACK. NDT TO DETERMINE LENGTH OF CRACK. STOP DRILLED AND NDT TO CONFIRM CRACK. STOP DRILLED - BROKEN SHARP EDGES. TREATED, PRIMED AND FILLED STOP DRILL HOLES WITH SEALER PER
- [SDR 99T64R535EWA](https://openairdocs.org/sdr/99T64R535EWA.md): Fastener · missing · Nov 11, 1999 · N8079U · Doug DC871 · Main Landing Gear Attach Section
  > FOUND DURING D-CHECK. RT MAIN LANDING GEAR FITTING MISSING FASTENER AFT SIDE. (EO). LEFT THE SHEARED SHANK IN THE HOLE, FILLED HOLE WITH PR1422B 1/2 SEAL. IT IS ACCEPTABLE TO RETURN TO SERVICE PER EO 99-174 WITH APPROVED 8110-3 DATED 11-11-99. REF: EME
- [SDR 99T64R539EWA](https://openairdocs.org/sdr/99T64R539EWA.md): Door · missing · Nov 10, 1999 · N8079U · Doug DC871 · Fixed Inner Doors
  > DURING D-CHECK. FABRICATED AND INSTALLED DIVIDER WALL BETWEEN C AND D PITS. (EO). FABRICATED A NEW DOOR USING DRAWING 99-174-2. TREATED AND PRIMED PER EO 999-174 WITH APPROVED 8110-3 DATED 11-8-99. REF: EMERY WORLDWIDE A/L. RRXA. (X)
- [SDR 99T64R534EWA](https://openairdocs.org/sdr/99T64R534EWA.md): Pin Boss · corroded · Nov 9, 1999 · N8079U · Doug DC871 · Landing Gear Retraction/Extension System
  > FOUND DURING D-CHECK. RT MAIN LANDING GEAR SHOCK STRUT ASSY RETRACT PIN BOSS CORRODED. (EO). BLENDED OUT CORROSION. FABRICATED NEW BUSHING AND CAD PLATED IAW EO 99-174 WITH APPROVED 8110-3 DATED 10-15-99. INSTALLED BUSHING AND PIN IAW DC-8 SB 32-102.
- [SDR 99T64R504EWA](https://openairdocs.org/sdr/99T64R504EWA.md): Drain Plug · missing · Nov 8, 1999 · N8079U · Doug DC871 · Cargo/Baggage Doors
  > FOUND DURING D-CHECK. C-PIT DOOR MISSING DRAIN PLUG. FABRICATED FILLER. TREATED AND PRIMED. INSTALLED FILLERS AND DRAIN PLUG PER EO 99-174 WITH APPROVED 8110-3 DATED 11-02-99. REF: EMERY WORLD WIDE A/L, RRXA. (X)
- [SDR 99T64R444EWA](https://openairdocs.org/sdr/99T64R444EWA.md): Bulkhead · damaged · Nov 4, 1999 · N8079U · Doug DC871 · Fuselage Main, Bulkhead
  > FOUND DURING D-CHECK. 'A' PIT AFT BULKHEAD BOTTOM NEEDS TO BE TRIMMED STA 440. (EO). FABRICATED NEW DOOR USING DRAWING NR 99-174-1. TREATED AND PRIMED IAW EO 99-174 WITH APPROVED 8110-3 DATED 10-20-99. REF: EMERY WORLDWIDE A/L. RRXA. (X)
- [SDR RRXA991790](https://openairdocs.org/sdr/RRXA991790.md): Floor Panel · corroded · Nov 3, 1999 · N8079U · Doug DC871F · Fuselage Floor Panel
  > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FLOOR PANEL BETWEEN STA 660 TO STA 750. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FLOOR PANEL IAW DC-8 SRM 53-2-3. CORROSION
- [SDR RRXA991789](https://openairdocs.org/sdr/RRXA991789.md): Floor Panel · corroded · Nov 3, 1999 · N8079U · Doug DC871F · Fuselage Floor Panel
  > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FLOOR PANEL BETWEEN STA 750 TO STA 860. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FLOOR PANEL IAW DC-8 SRM 53-2-3. CORROSION
- [SDR RRXA991788](https://openairdocs.org/sdr/RRXA991788.md): Floor Panel · corroded · Nov 3, 1999 · N8079U · Doug DC871F · Fuselage Floor Panel
  > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FLOOR PANEL BETWEEN STA 40 TO STA 80 AND BETWEEN BL 56L TO BL 68L. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FLOOR PANEL IAW
- [SDR RRXA991787](https://openairdocs.org/sdr/RRXA991787.md): Floor Panel · corroded · Nov 3, 1999 · N8079U · Doug DC871F · Fuselage Floor Panel
  > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FLOOR PANEL BETWEEN STA 1240 TO STA 1348 AND BETWEEN BL 48L TO BL 62L. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FLOOR PANEL
- [SDR RRXA991786](https://openairdocs.org/sdr/RRXA991786.md): Floor Panel · corroded · Nov 3, 1999 · N8079U · Doug DC871F · Fuselage Floor Panel
  > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FLOOR PANEL BETWEEN STA 340 TO STA 346. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FLOOR PANEL IAW DC-8 SRM 53-2-3. CORROSION
- [SDR 99T64R537EWA](https://openairdocs.org/sdr/99T64R537EWA.md): Panel · broken · Nov 3, 1999 · N8079U · Doug DC871 · Fuselage Miscellaneous Structure
  > FOUND DURING D-CHECK. STA 1660 SIDE RAIL PANEL BROKEN STA 1650 - STA 1700. (EO). FABRICATED NEW SIDE RAIL PANEL PER EO 99-174 WITH APPROVED 8110-3 DATED 10-20-99. REF: EMERY WORLDWIDE A/L. RRXA. (X)
- [SDR RRXA991779](https://openairdocs.org/sdr/RRXA991779.md): Frame · corroded · Nov 2, 1999 · N8079U · Doug DC871F · Fuselage Main, Frame
  > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FRAME AT STA=-69 BETWEEN BL=0 TO BL=45L AND WL-9.5. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR SPLICE IAW FAA APPROVED DER
- [SDR 99T64R532EWA](https://openairdocs.org/sdr/99T64R532EWA.md): Vane · damaged · Oct 27, 1999 · N8079U · Doug DC871 · Trailing Edge Flaps
  > FOUND DURING D-CHECK. RIGHT OUTBOARD FLAP NR 5 VANE INBOARD UPPER END HAS ELONGATED HOLE. DRILLED AND REAMED HOLE TO.75 INCH DIAMETER. TREATED AND PRIMED. FABRICATED PLUG AND INSTALLED, DRILLED PLUG TO CORRECT HOLE SIZE PER EO 99-174 WITH APPROVED 8110-3
- [SDR 99T64R518EWA](https://openairdocs.org/sdr/99T64R518EWA.md): Skin · damaged · Oct 27, 1999 · N8079U · Doug DC871 · Trailing Edge Flaps
  > FOUND DURING D-CHECK. LEFT WING OUTBOARD FLAP VANE INBOARD END UPPER SURFACE HAS IMPROPER REPAIR OF ELONGATED HOLE. DRILLED AND REAMED HOLE TO.375 INCH DIAMETER. FABRICATED PLUG AND INSTALLED PER EO 99-174 WITH APPROVED 8110-3 DATED 9-21-99. REF: EMERY W
- [SDR 99T64R452EWA](https://openairdocs.org/sdr/99T64R452EWA.md): Actuator Crank · cracked · Oct 26, 1999 · N8079U · Doug DC871 · Trailing Edge Flaps
  > FOUND DURING D-CHECK. RIGHT WING FLAP ACTUATOR ASSY STA 340 FOUND CRANK TO BE CRACKED. REMOVED AND REPLACED CRACK ON FLAP ACTUATOR ASSEMBLY IAW DC-8 OHM 27-28-7. REF: EMERY WORLD WIDE A/L, RRXA. (X)
- [SDR 99T64R451EWA](https://openairdocs.org/sdr/99T64R451EWA.md): Actuator Crank · cracked · Oct 26, 1999 · N8079U · Doug DC871 · Trailing Edge Flaps
  > FOUND DURING D-CHECK. LT WING FLAP ACTUATOR ASSY STA 340 FOUND CRANK TO BE CRACKED. REMOVED AND REPLACED CRANK ON FLAP ACTUATOR ASSY IAW DC-8 OHM 27-28-7. REF: EMERY WORLDWIDE A/L. RRXA. (X)
- [SDR 99T64R503EWA](https://openairdocs.org/sdr/99T64R503EWA.md): Skin · damaged · Oct 25, 1999 · N8079U · Doug DC871 · Trailing Edge Flaps
  > FOUND DURING D-CHECK. RIGHT OUTBOARD FLAP NR 6 VANE INBOARD END TOP SIDE HAS HOLE ELONGATED. DRILLED AND REAMED HOLE TO.375 INCH. FABRICATED PLUG AND INSTALLED PER EO 99-174 WITH APPROVED 8110-3 DATED 9-21-99. REF: EMERY WORLD WIDE A/L, RRXA. (X)
- [SDR RRXA991780](https://openairdocs.org/sdr/RRXA991780.md): Intercostal · corroded · Oct 22, 1999 · N8079U · Doug DC871F · Fuselage Miscellaneous Structure
  > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO INTERCOSTAL BETWEEN STA 980 TO STA 995 AND LONGERON 35 LEFT. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW INTERCOSTAL IAW DC-8 S
- [SDR 99T64R536EWA](https://openairdocs.org/sdr/99T64R536EWA.md): Skin · damaged · Oct 22, 1999 · N8079U · Doug DC871 · Wing, Plate/Skin
  > RIGHT INBOARD LEADING EDGE TOP MOUNT HOLES DAMAGED OR ELONGATED, 7 EACH. DRILLED, PRIMED AND INSTALLED IAW EO NR 99-174 WITH APPROVED 8110-3 DATED 9-14-99. REF: EMERY WORLD WIDE A/L, RRXA. (X)
- [SDR 99T64R538EWA](https://openairdocs.org/sdr/99T64R538EWA.md): Kick Plate · cracked · Oct 18, 1999 · N8079U · Doug DC871 · Fuselage Miscellaneous Structure
  > FOUND DURING D-CHECK. AFT LOWER CARGO RACKS AND DENTS. (EO). STRAIGHTEN DENTS. NDT VERIFIED NO CRACKS, STOP DRILLED CRACKS AND WELDED IAW EO 99-174 WITH APPROVED 8110-3 DATED 10-11-99. REF: EMERY WORLDWIDE A/L. RRXA. (X)
- [SDR 99T64R513EWA](https://openairdocs.org/sdr/99T64R513EWA.md): Thrust Reverser · damaged · Oct 18, 1999 · N8079U · Doug DC871 · Engine Thrust Reverser
  > FOUND DURING D-CHECK. RT FAN REV DAMAGED ON LOWER VERTICAL SURFACE. CUT OUT DAMAGED AREA, FILLED WITH LY5052 02 RESIN AND HY5052 02 RESIN CATALYST MIXED WITH MICRO BALLOONS. FABRICATED DOUBLER AND INSTALLED PER EO 99-174 WITH APPROVED 8110-3 DATED 10-01-99.
- [SDR 99T64R512EWA](https://openairdocs.org/sdr/99T64R512EWA.md): Cowl · damaged · Oct 18, 1999 · N8079U · Doug DC871 · Engine Cowling System
  > FOUND DURING D-CHECK. HOLE ON INSIDE OF LT FORWARD OF LT FORWARD COWL NR 1 ENGINE. CUT OUT DAMAGED AREA, FILLED WITH LY5052 02 RESIN AND HY5052 02 RESIN CATALYST AND MIRCO BALLONS. FABRICATED DOUBLER AND INSTALLED PER EO 99-174 WITH APPROVED 8110-3 DATED 10
- [SDR 99T64R508W](https://openairdocs.org/sdr/99T64R508W.md): Kick Plate · damaged · Oct 18, 1999 · N8079U · Doug DC871 · Fuselage Miscellaneous Structure
  > FOUND DURING D-CHECK. TYPE ONE EMERGENCY EXIT DOOR LEFT SIDE. KICK PLATE DAMAGED. (EO). STOP DRILLED CRACK, NDT TO ASSURE CRACKS HAD BEEN STOPPED. WELDED KICK PLATE AND NDT TO ASSURE NO FLAWS IN WELD, NONE NOTED. PER EO 99-174 WITH APPROVED 8110-3 DATED
- [SDR 99T64R434EWA](https://openairdocs.org/sdr/99T64R434EWA.md): Stiffener · broken · Oct 18, 1999 · N8079U · Doug DC871 · Fuselage Miscellaneous Structure
  > LEFT WHEELWELL FORWARD WEBBING FRAME BROKEN. (EO). WELDED NEW SECTION OF TUBING PER MIL-STD-2219. NDT WELD NO FLAWS FOUND. ACCEPTABLE TO RETURN TO SERVICE PER EO NR 99-174 WITH APPROVED 8110-3 DATED 9-24-99. REF: EMERY WORLD WIDE A/L, RRXA. (X)
- [SDR 99T64R432EWA](https://openairdocs.org/sdr/99T64R432EWA.md): Stiffener · broken · Oct 18, 1999 · N8079U · Doug DC871 · Fuselage Miscellaneous Structure
  > RIGHT WHEELWELL FORWARD WEBBING STIFFENER BROKEN. (EO). WELDED NEW SECTION OF TUBING IAW MIL-STD-2219. NDT WELD NO FLAWS FOUND PER EO NR 99-174 WITH APPROVED 8110-3 DATED 9-21-99. REF: EMERY WORLD WIDE A/L, RRXA. (X)
- [SDR 99T64R514EWA](https://openairdocs.org/sdr/99T64R514EWA.md): Line · chafed · Oct 15, 1999 · N8079U · Doug DC871 · Extinguishing System
  > FOUND DURING D-CHECK. FIRE RETARDANT LINE CHAFED FORWARD OF TOMBSTONE NR 3 PYLON. BLENDED CHAFE SMOOTH FILLED CHAFE WITH WELD, NDT WELD NO FLAWS FOUND PER EO 99-174 WITH APPROVED 8110-3 DATED 10-7-99. REF: EMERY WORLD WIDE A/L, RRXA. (X)
- [SDR 99T64R510EWA](https://openairdocs.org/sdr/99T64R510EWA.md): Kick Plate · damaged · Oct 14, 1999 · N8079U · Doug DC871 · Fuselage Miscellaneous Structure
  > FOUND DURING C-CHECK. TYPE ONE EMERGENCY DOOR RIGHT FORWARD KICKPLATE DAMAGED. (EO). STOP DRILLED CRACK, NDT TO ASSURE CRACKS HAVE BEEN STOPPED, WELDED KICKPLATE AND NDT TO ASSURE NO FLAWS IN WELD, NONE NOTED. PER EO 99-174 WITH APPROVED 8110-3 DATED 10-14
- [SDR 99T64R509EWA](https://openairdocs.org/sdr/99T64R509EWA.md): Kick Plate · damaged · Oct 14, 1999 · N8079U · Doug DC871 · Fuselage Miscellaneous Structure
  > FOUND DURING D-CHECK. TYPE ONE EMERGENCY DOOR AFT RIGHT SIDE KICKPLATE DAMAGED. (EO). STOP DRILLED CRACK, NDT TO ASSURE CRACKS HAD BEEN STOPPED. WELDED KICKPLATE AND NDT TO ASSURE NO FLAWS IN WELD, NONE NOTED. PER EO 99-174 WITH APPROVED 8110-3 DATED 10-
- [SDR 99T64R507EWA](https://openairdocs.org/sdr/99T64R507EWA.md): Kick Plate · gouged · Oct 12, 1999 · N8079U · Doug DC871 · Fuselage Miscellaneous Structure
  > FOUND DURING D-CHECK. B-PIT DOOR KICK PLATE GOUGED/SCRATCHED. (EO). FABRICATED NEW KICK PLATE. WELDED ACCORDING TO MIL-STD-2219, NDT WELD TO ASSURE NO FLAWS IN WELD. NONE NOTED, AND INSTALLED PER EO 99-174 WITH APPROVED 8110-3 DATED 9-20-99. REF: EMERY
- [SDR 99T64R454EWA](https://openairdocs.org/sdr/99T64R454EWA.md): Skin · damaged · Oct 12, 1999 · N8079U · Doug DC871 · Wing, Plate/Skin
  > FOUND DURING D-CHECK. RT MID LEADING EDGE TWO DOUBLER LOWER EXTERIOR TO EVALUATE DAMAGE STA XFS 416.500 - XS 435.289. (EO). REMOVED AND REPLACED THE OUTBOARD EXTERNAL SKIN WITH NEW SKIN SAME SIZE. SHAPE AND MATERIAL AS THE ORIGINAL PER EO 99-174 WITH APROVE
- [SDR RRXA991785](https://openairdocs.org/sdr/RRXA991785.md): Intercostal · corroded · Oct 8, 1999 · N8079U · Doug DC871F · Fuselage Miscellaneous Structure
  > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO INTERCOSTAL BETWEEN STA 520 TO STA 540 AND LONGERON 32 RIGHT. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW INTERCOSTAL IAW DC-8
- [SDR 99T64R515EWA](https://openairdocs.org/sdr/99T64R515EWA.md): Thrust Reverser · lightning strike · Oct 8, 1999 · N8079U · Doug DC871 · Engine Thrust Reverser
  > FOUND DURING D-CHECK. THREE LIGHTNING STRIKES, RIGHT FAN REV. TRAILING EDGE OUTER SECTION MIDDLE AND BOTTOM NR 4 ENGINE. (EO). BLENDED THE EDGE OF THE LIGHTNING STRIKES, SMOOTH, ALODINED AND FINISHED PER FACTORY SPECS. IT IS ACCEPTABLE TO RETURN TO SERVIC
- [SDR 99T64R453EWA](https://openairdocs.org/sdr/99T64R453EWA.md): Skin · damaged · Oct 8, 1999 · N8079U · Doug DC871 · Wing, Plate/Skin
  > FOUND DURING D-CHECK, LT MID-WIND LEADING EDGE OUTBOARD END SLOT VANE STA 520.168, HOLES WORN AND ELONGATED. (EO). FABRICATED REPAIR STRAP 12 INCHES BY 2.25 INCHES. TREATED AND PRIMED. INSTALLED CONICAL WASHERS AND INSTALLED REPAIR STRAP PER EO 99-174 WITH
- [SDR 99T64R445EWA](https://openairdocs.org/sdr/99T64R445EWA.md): Bushing Mount · cracked · Oct 7, 1999 · N8079U · Doug DC871 · Fuselage Miscellaneous Structure
  > FOUND DURING D-CHECK. AFT PASSENGER DOOR (L2) HAS CRACK AT UPPER HINGE BUSHING AREA STA 1600. REMOVED CRACK SECTION BY CUT OUT. FABRICATED REPAIR DOUBLERS. TREATED, PRIMED, AND INSTALLED PER EO 99-174 WITH APPROVED 8110-3 DATED 10-01-99. REF: EMERY WORL
- [SDR 99664R428EWA](https://openairdocs.org/sdr/99664R428EWA.md): Skin · damaged · Oct 7, 1999 · N8079U · Doug DC871 · Fuselage Main, Plate/Skin
  > EXTERIOR RT LIGHTING STRIKE STA 250 RT BETWEEN L21R - L22R. (EO). BLENDED ROUGH AREAS SMOOTH, REAMED HOLES AND INSTALLED MS20470AD8 RIVET. TREATED AND PRIMED PER EO 99-174 WITH APPROVED 8110-3 DATED 9-16-99. REF: EMERY WORLDWIDE A/L. RRXA. (X)
- [SDR RRXA991781](https://openairdocs.org/sdr/RRXA991781.md): Frame · corroded · Oct 6, 1999 · N8079U · Doug DC871F · Fuselage Main, Frame
  > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FRAME AT STA 1280 AND LONGERON 35 LEFT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR SPLICE IAW DC-8 SRM 51-1-21. CORROSION D
- [SDR 99T64R500EWA](https://openairdocs.org/sdr/99T64R500EWA.md): Cover · gouged · Oct 6, 1999 · N8079U · Doug DC871 · Fuselage Miscellaneous Structure
  > FOUND DURING D-CHECK. 'D' PIT DOOR THRESHOLD PLATE GOUGED/SCRATCHED STA 1420. (EO). REMOVED THE EXISTING D-PIT THRESHOLD PLATE. FABRICATED NEW THRESHOLD, WELDED CURVED PORTIONS AND NDT WELDS. NO FLAWS FOUND AND INSTALLED PER EO 99-174 WITH APPROVED 8110-3
- [SDR 99T64R506EWA](https://openairdocs.org/sdr/99T64R506EWA.md): Frame · corroded · Oct 5, 1999 · N8079U · Doug DC871 · Fuselage Main, Frame
  > FOUDN DURING D-CHECK. CORROSION AT STA -67 APPROXIMATELY 45 INCHES LEFT OF CENTER ON SUB-FLOOR FRAME IN COCKPIT. (EO). REMOVED CORROSION. TREATED, PRIMED AND FINISHED PER FACTORY SPECIFICATIONS. FABRICATED REPAIR ANGLE AND INSTALLED PER EO 99-174 WITH APP
- [SDR 99T64R455EWA](https://openairdocs.org/sdr/99T64R455EWA.md): Skin · lightning strike · Oct 4, 1999 · N8079U · Doug DC871 · Wing, Plate/Skin
  > FOUND DURING D-CHECK. LIGHTNING STRIKE STA 300 RT BETWEEN L18R - L19R (EO). OPENED LIGHTNING STRIKE HOLE TO.375 INCH. FABRICATED DOUBLER AND INSTALLED PER EO 99-174 WITH APPROVED 8110-3 DATED 10-4-99. REF: EMERY WORLD WIDE A/L, RRXA. (X)
- [SDR RRXA991783](https://openairdocs.org/sdr/RRXA991783.md): Bolt · corroded · Oct 3, 1999 · N8079U · Doug DC871F · Cargo/Baggage Doors
  > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO CARGO DOOR T-BOLT BETWEEN STA 280 TO STA 340 AND LONGERON 29 RIGHT. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED NEW T-BOLT AND INSTALLED DC-8 SRM 5
- [SDR 99T64R440EWA](https://openairdocs.org/sdr/99T64R440EWA.md): Rib · cracked · Oct 2, 1999 · N8079U · Doug DC871 · Wing, Rib/Bulkhead
  > LEFT WING T/E STA 261 FLAP WELL RIB CRACKED BELOW NR 4 SPOILER. CUT OUT CRACK. TREATED AND PRIMED. FABRICATED REPAIR DOUBLER AND INSTALLED PER EO NR 99-174 WITH APPROVED 8110-3 DATED 9-21-99. REF: EMERY WORLD WIDE A/L, RRXA. (X)
- [SDR RRXA991784](https://openairdocs.org/sdr/RRXA991784.md): Frame · corroded · Oct 1, 1999 · N8079U · Doug DC871F · Fuselage Main, Frame
  > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FRAME AT STA 1420 AND LONGERON 36. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR SPLICE IAW DC-8 SRM 53-2-0. CORROSION DAMAGE
- [SDR 99T64R426EWA](https://openairdocs.org/sdr/99T64R426EWA.md): Seat Tracks · worn · Oct 1, 1999 · N8079U · Doug DC871 · Fuselage, Seat/Cargo Attach Fittings
  > F/E SEAT AFT TRACK LOCK HOLES WORN TO LIMITS. REMOVED AND REPLACED F/E'S SEAT TRACK IAW DC-8 SRM 51-1-21. REF: EMERY WORLDWIDE A/L. RRXA. (X)
- [SDR 99T64R475EWA](https://openairdocs.org/sdr/99T64R475EWA.md): Skin · damaged · Sep 28, 1999 · N8079U · Doug DC871 · Wing, Plate/Skin
  > FOUND DURING D-CHECK, MID-WING LEADING EDGE SLOT VANE HOLE OVERSIZED AND WORN AT STA XS 520.186. (EO). CLEANED EXISTNG COUNTERSINKS, ALODINED, TREATED AND PRIMED. FABRICATED CONICAL WASHERS AND FILLED THE COUNTERSINKS. FABRICATED REPAIR DOUBLER AND INSTALL
- [SDR 99T64R429EWA](https://openairdocs.org/sdr/99T64R429EWA.md): Shim · broken · Sep 25, 1999 · N8079U · Doug DC871 · Leading Edge Devices
  > NR 3 STUB WING L/E INBOARD LOWER SPAR CAP SHIM BROKEN OFF XILD.7095. (EO). SMOOTHED REMAINING EDGE OF SHIM. NDT TO ASSURE THAT NO CRACKS EXIST. (NONE FOUND). TREATED AND PRIMED, INSTALLED INBOARD PIECE AS A SHIM USE FACTORY FASTENERS PER EO 99-174 WITH A
- [SDR RRXA991782](https://openairdocs.org/sdr/RRXA991782.md): Finger Doubler · corroded · Sep 24, 1999 · N8079U · Doug DC871F · Fuselage Miscellaneous Structure
  > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FINGER DOUBLER AT STA -25 AND BL 36L AND WL -9. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FINGER DOUBLER IAW DC-8 SRM 53-3-1.
- [SDR 99T64R467WEA](https://openairdocs.org/sdr/99T64R467WEA.md): Rib · cracked · Sep 23, 1999 · N8079U · Doug DC871 · Wing, Rib/Bulkhead
  > FOUND DURING D-CHECK. NR 2 STUB WING LEADING EDGE, 7 INCH CRACK TOP RIB STA 250.089. STOP DRILLED CRACK IAW DC-8 SRM 57-2-0. FABRICATED TWO DOUBLERS IAW DC-8 SRM 57-2-0. TREATED AND PRIMED IAW DC-8 SRM 51-1-8. INSTALLED DOUBLERS IAW DC-8 SRM 51-1-20D AND

Next page: https://openairdocs.org/deregistered/N8079U-2001-09-06/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE n_number = 'N8079U' AND deregistration_id = 'N8079U-2001-09-06'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N8079U-2001-09-06/reports

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